You are not logged in (Log in). A3M14AML – Aerodynamics and mechanics of flight – B Home · Courses · A3M14AML – Aerodynamics and mechanics of. Home; /; aerodynamika a mechanika letu pro piloty a techniky pdf zip, found for you zslg. Deprecated: Non-static method JSite::getMenu() should not be called. Komplexní znalost letounu v kombinaci s nejnovějšími výpočtovými metodami nám umožňuje zvýšit rychlost a zlepšit výkony stroje. Mechanika letu & výkony.

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Longitudinal and lateral-directional static stability. Flight mechanics is a follow up to the first part of the course. Individual tasks must be finished and handed in the week credits are awarded as the latest. Familiarizing students with the method of assessment of classical theory of performance and a judgment of aerodynamic and propulsion characteristics efficiency on flight performance.

The basics of thermomechanics, 1st and 2nd Laws. Planned learning activities and teaching methods. Evaluation fulfils the University requirements.

Longitudinal and lateral-directional dynamic stability. Type of course unit. Boundary layers, airfoils, polar curve, influence of Reynolds number.

Index of /AK_Slany/svazarm/Aerodynamika_a_mechanika_letu/

Take-off and landing performance. Supersonic flow, supersonic continuous expansion, shock waves. Subsonic flow around airfoils and wings.


Conservation laws, stream lines, equations of continuity and Bernoulli, speed measurement, aerodynamic forces. The basics of common mechanics — force effect on a body, kinematics, dynamics.

Finite span wing, induced drag, high lift devices, spoilers, vortex generators. Recommended optional programme components.

Performance requirements of JAR standards. The course offers for students the knowledge necessary for an dynamic stability modes estimation and their influence aerodynmaika aircraft handling, longitudinal and lateral-directional stability.

Familiarizing students with the methods of calculation of the stability and aircraft control. Students will also learn to judge the influence of aircraft design parameters on its flying characteristics. Lateral-directional control of airplane. Learning outcomes of the course unit. Calculatipon of stall and maximum speeds.

Conditions to obtain the course-unit credit: Determination of the basic technical aircraft data in the classic aircraft performance and stability and control. Boundary layers, origin of lift, airfoils, finite span wings, induced drag, high lif devices.

Aerodynamics and Flight Mechanics

Steady climbing and gliding flight. Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations. Further they will have a clear idea of range and endurance, take-off and landing operations, classical theory of the stability and control of aircraft, development of general equations of motion for an atmospheric aircraft, classical small petu equations of motion, aircraft state equations.


Qualitative and quantitative appraisal of aircraft performance and stability and control regarding the design and optimal use of an aircraft. Steady turning performance calculation.

Course detail – Aerodynamics and Flight Mechanics () – BUT

Specification of controlled education, way of implementation and compensation for absences. Thrust and power diagram calculation. Assesment methods and mdchanika linked to learning outcomes. Control-fixed neutral point and manoeuvre point of airplane calculation. Measurement of pressure distribution at airfoil surface. Recommended or required reading.

Limitations of turning flight. Performance in horizontal flight, performance at climbing and gliding, performance at turning flight are included. Airfoils, wing of finite span. The exam has written the essential one and oral parts.

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